# Service difficulty reports: N641UA

A list on [N641UA](https://openairdocs.org/aircraft/N641UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 311 reports

- [SDR CALA2026101520364](https://openairdocs.org/sdr/CALA2026101520364.md): Unknown · odor · Oct 11, 2026 · N641UA · Boeing 767322 · Air Distribution System
  > DUE TO REPORTED STRONG BURNING ODOR IN AIRCRAFT. COMPLY WITH CONDITIONAL INSPECTION AMM TASK 05-51-56-940-801-C1. CREW WAS DEBRIEFED AND FORM EMAILED TO TOMC, NO POSITIVE SOURCE OF THE ODOR WAS IDENTIFIED DURING CREW DEBRIEF. CONDITIONAL INSPECTION C/W IAW A
- [SDR CALA2026101320353](https://openairdocs.org/sdr/CALA2026101320353.md): Unknown · odor · Oct 10, 2026 · N641UA · Boeing 767322 · Air Distribution System
  > STRONG BURNING ODOR THROUGHOUT ACFT FOLLOWING START OF LT ENG. NO SMOKE PRESENT. APU BLEED ON. ISOLATION VALVES OPEN. PACKS OFF. REMAINED STRONG BY EXIT ROWS. NOTICED STRONG OIL ODOR FROM NR 1 ENG EXHAUST WHEN FIRST ARRIVED AT PLANE BUT NO SMOKE. NO OBVIO
- [SDR CALA2026091419410](https://openairdocs.org/sdr/CALA2026091419410.md): Light · broken · Sep 11, 2026 · N641UA · Boeing 767322 · Emergency Lighting
  > GENERAL VISUAL INSPECTION OF THE BE PINNACLE TOURIST SEAT. FOUND EMERGENCY PATH LIGHTS BROKEN AT POSITIONS 30D, 33D, 43D AND 50D BROKEN. REMOVED AND REPLACED EMERGENCY PATH LIGHTS ATE SEATS 30D, 33D,43D AND 50D REF. AMM TASK: 33-51-00/501, OPS GOOD.
- [SDR CALA2026052816593](https://openairdocs.org/sdr/CALA2026052816593.md): Bulb · faulted · May 26, 2026 · N641UA · Boeing 767322 · Passenger Compartment Lighting
  > SEAT 43L OVERHEAD LIGHT BULB OVERHEATED AND STARTED TO SMOKE..FA. SHUT IT OFF. MOVED PAX TOO. PERFORMED 15 MINUTE OPS CHECK OF THE READING LIGHTS, SIDEWALL, LIGHTS & OVERHEAD LIGHTS. NO SMOKE WAS DETECTED. ALL LIGHTS ARE WORKING. NO FURTHER ACTION REQUIRED
- [SDR CALA2025112811543](https://openairdocs.org/sdr/CALA2025112811543.md): Display · malfunctioned · Nov 22, 2025 · N641UA · Boeing 767322 · Indicating/Recording System
  > IFE SCREEN IS INTERMIT ENT. GOES BACK AND FORTH BETWEEN STARTUP AND SHUTDOWN. FA REPORTS CREW TERMINAL IS GHOSTING AND SELECTS ITEMS WITH NO COMMAND. CLEANED SCREEN, COULD NOT REPLICATE FAULT. IFE SYS OPS CHK GOOD. REF 44-25-00
- [SDR CALA2025093009430](https://openairdocs.org/sdr/CALA2025093009430.md): Skin · ground damage · Sep 28, 2025 · N641UA · Boeing 767322 · Fuselage Main, Plate/Skin
  > LOADER CAME IN CONTACT WITH THE ACFT AT THE AFT CARGO DOOR, DAMAGE IS LOCATED APPROX. BS 1373, ABOVE STRINGER 29R ON FUSELAGE SKIN WITH PULLED FASTENERS ON SKIN. INSPECTION OF UNDERLYING STRUCTURE REVEALED BOWED FRAME. DAMAGE DEMENSIONS ARE 3.6"X 1.1". BLEN
- [SDR CALA2025093009428](https://openairdocs.org/sdr/CALA2025093009428.md): Shear Tie · damaged · Sep 28, 2025 · N641UA · Boeing 767322 · Fuselage Internal Mounting Structure
  > WHEN REMOVING DAMAGED SHEAR TIE FOUND DAMAGE TO FRAME AT BS 1373 BETWEEN S-28R AND S-27R, ACCOMPLISHED HFEC OF CUT OUT AREA STEP 7 REF AVO 15518 REV A. NO CRACKS INDICATED. REF AVO 15518 REV A. COMPLIED WITH STEP 8 WITH A.040 INSURANCE CUT. COMPLETED STES
- [SDR CALA2025081807885](https://openairdocs.org/sdr/CALA2025081807885.md): Cable · disconnected · Aug 14, 2025 · N641UA · Boeing 767322 · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE DEPLOYMENT CABLE FOUND DISCONNECTED FROM GIRT BAR. UPON FURTHER INVESTIGATION WITH SLIDE REMOVED FOUND GIRT BAR OUTSIDE OF GIRT BAR HOLDER. REMOVED AND INSPECTED SLIDE NO DAMAGE FOUND, REINSTALLED L1 DOOR SLIDE REF AMM 25-66-01-404-072. C/
- [SDR CALA2025081107529](https://openairdocs.org/sdr/CALA2025081107529.md): Unknown · odor · Aug 9, 2025 · N641UA · Boeing 767322 · Air Distribution System
  > BURNING ODOR IN AFT GALLEY AND FA REPORTED UNUSUAL SOUND. REMOVED ALL CARTS FROM AFT GALLEY TO PERFORM A DETAILED INSPECTION IAW AMM 25-31-91-202-001 AND CHECKED OVENS FOR DEFECTS OR ANY BURNING. OPERATED CHILLERS FOR 15MINS IAW AMM 25-31-00-705-001 AND 25-33
- [SDR CALA2025031902939](https://openairdocs.org/sdr/CALA2025031902939.md): Slide · not reported · Mar 16, 2025 · N641UA · Boeing 767324 · Escape Slide
  > FOR TRACKING PURPOSES INFORMATION ONLY, L1 DOOR ESCAPE SLIDE REPLACEMENT SCHEDULED UPDATING SERVICEABLE PARTS TAG FOR L1 DOOR ESCAPE SLIDE TRACKING TAG # 1425358, AS REQUIRED. PARTS USED: 76-2500-9-0001, QTY:1 ROTABLE PARTS CHG:TT # 1425358 SN OFF 1495 PN OFF
- [SDR CALA2025031702865](https://openairdocs.org/sdr/CALA2025031702865.md): Shroud · damaged · Mar 14, 2025 · N641UA · Boeing 767322 · Emergency Lighting
  > SEAT 48F EMERGENCY EXIT LIGHT DAMAGED REMOVED AND REPLACED DAMAGED LIGHT ASSEMBLY REF IFM 25-21-53.
- [SDR CALA2025030302562](https://openairdocs.org/sdr/CALA2025030302562.md): Chiller · smoke · Mar 2, 2025 · N641UA · Boeing 767322 · Buffet/Galleys
  > AFT CHILLERS SMOKING WITH SMELL REF TO LP 4024883 THIS CHILLER WAS REPLACED FOR THE SAME ISSUES.. REF LOGPAGE 4024883, ISOLATED ISSUE TO AFT GALLEY UPPER CHILLER. INSPECTED BOTH UPPER AND LOWER CANNON PLUGS AND ASSC'D WIRE HARNESSES FOR SIGNS OF BURNING OR ARC
- [SDR CALA2025030402587](https://openairdocs.org/sdr/CALA2025030402587.md): Chiller · faulty · Feb 28, 2025 · N641UA · Boeing 767322 · Buffet/Galleys
  > AFT CHILLERS CAUSING SMOKE CB PULLED SMOKE AND ELECTICAL ODOR DISAPATED VERIFIED NO SMOKE OR ODOR WITH CHILLER DEACTIVATED REQ TOMC APRVL TO DEF BOTH CHILLER IN AFT GALLEY DDP C/W CB PULLED AND SECURED NOC.NEF 2520NB APPROVED DEFERRED AFT GALLEY CHILLER PER N
- [SDR CALA2025030302533](https://openairdocs.org/sdr/CALA2025030302533.md): Oven · odor · Feb 28, 2025 · N641UA · Boeing 767322 · Buffet/Galleys
  > ON ARIVAL AT 18K AFT FA REPORTED SMOKE IN AFT GALLY. SHUT OFF OVEN AND IT GOT BETER DEBRIEFED FLT AND CABIN CREW, ELECTRICAL SMELL NOTICED IN AFT GALLEY AREA AND MORE NOTICEABLE ABOVE AFT CTR F/A SEATS. MX DID NOT SEE OR SMELL ANYTHING UNUSUAL IN ACFT AND ALL
- [SDR CALA2025030302530](https://openairdocs.org/sdr/CALA2025030302530.md): Unknown · odor · Feb 28, 2025 · N641UA · Boeing 767322 · Air Distribution System
  > SMOKE AFT GALLEY, REF LOG 4015078. LOG NEEDS TO BE SIGNED OF WITH REFERENCE TO CONDITIONAL INSPECTION SMOKE OR ODOR IN THE FLIGHT DECK AND OR CABIN, AMM 05-51-56/201 CONDITIONAL INSPECTION COMPLIED ON LP 4015078
- [SDR CALA2024121701553](https://openairdocs.org/sdr/CALA2024121701553.md): Ceiling Panel · out of position · Dec 15, 2024 · N641UA · Boeing 767322 · Passenger Compartment Equipment
  > LEFT AFT ENTRY DOOR ON EICAS. CLOSED SENSOR S204 SHOWING FAR WITH DOOR VERIFIED CLOSED. REPOSITIONED MOVABLE CEILING PANEL, ALL INDICATIONS NOW GOOD. VERIFIED DOOR OPEN CLOSED OPERATION. CLOSED SENSOR S204 SHOWING FAR WITH DOOR VERIFIED CLOSED. REPOSITIONED M
- [SDR CALA2024120501415](https://openairdocs.org/sdr/CALA2024120501415.md): Snubber · faulty · Dec 2, 2024 · N641UA · Boeing 767322 · Passenger/Crew Doors
  > L AFT ENT DOOR EICAS.SENSOR FOR AFT LEFT DOOR SHOWS. NEED SECOND DEFERRAL MEL CARD 33260 TARGET SHOWS FAR UNABLE TO DO PSEU SENSOR TEST TO CHECK SENSOR POSITION. UPON INSPECTION OF DOOR LATCHING MECHANISM, FOUND DOOR LATCH PIN DOES NOT EXTEND FULLY INTO LATCH
- [SDR CALA2024112601310](https://openairdocs.org/sdr/CALA2024112601310.md): Sign · detached · Nov 25, 2024 · N641UA · Boeing 767322 · Emergency Lighting
  > OVERWING EMERG. EXIT SIG N FALLING OFF AT SEATS 30 F-K EMERGENCY SIGN WAS REINSTALLED INTO PLACE OPS OK FOR SERVICE
- [SDR CALA2024112201243](https://openairdocs.org/sdr/CALA2024112201243.md): Unknown · odor · Nov 21, 2024 · N641UA · Boeing 767322 · Air Distribution System
  > STRONG SCENT OF ELEC SMOKE IN COCKPIT PERFORM AMM 05-51-56-940-801-C1 OF INTIAL INSPECTION UP TO AND INCLUDING 1.D.(8). FOUND NO SIGNS OF SMOKE OR SMOKE SMELL.
- [SDR CALA2024112201244](https://openairdocs.org/sdr/CALA2024112201244.md): Unknown · odor · Nov 20, 2024 · N641UA · Boeing 767322 · Air Distribution System
  > FLIGHT ATTENDANTS INFORM ED US THEY COULD SMELL SMOKE THROUGHT T HE CABIN AND IN THE AFT GALLEY PERFORMED INSPECTION REF AMM 05-51-56-940-801-C1. COMPLETED INSPECTION UP TO STEP 1.D.8 NO SIGNS OF SMOKE OR DAMAGE.
- [SDR CALA2024110102767](https://openairdocs.org/sdr/CALA2024110102767.md): Controller · inoperative · Oct 29, 2024 · N641UA · Boeing 767322 · Pneumatic Distribution System
  > R HPSOV EICAS CAUTION ON TAKEOFF PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST REF AMM 36-23-00. REMOVED HPSOV FOR REPLACEMENT. REF AMM 36-11-07 PERFORMED FIM 36-10 FT 865. ALL BLOCKS PASSED. BLOCK 6 SHOWED BITE TEST SHOWS HPSOV AND HPC FAULT. THE VERIFY TEST
- [SDR CALA2024101700849](https://openairdocs.org/sdr/CALA2024101700849.md): Transmitter · faulted · Oct 14, 2024 · N641UA · Boeing 767322 · Hydraulic Indicating System
  > L HYD QTY EICAS STATUS PG SHOWED 0.0RF OVRHD PANEL QYT LT TROUBLESHOT PER FIM 29-11 TREE 823. COMPARED HYD QUANTITY READING IN FLIGHT DECK WITH READING ON REMOTE SERVICING PANEL. READINGS WITHIN LIMITS. REMOVED AND REPLACED HYDRAULIC FLUID QUANTITY MONITORING
- [SDR CALA2024071800244](https://openairdocs.org/sdr/CALA2024071800244.md): Pump · unknown · Jul 16, 2024 · N641UA · Boeing 767322 · Standard Practices/Structures
  > R ELEC HYD DEMAND PUMP AUTO INOP THE PUMP RH DEMAND OPS NORMAL IN ON POSITION. REQUEST DEFERRAL MEL 2911K APPROVED FOR MEL 2911K PLACED RH ELEC HYD DEMAND PUMP ON MEL 2911K AS REQUESTED. DDP FOLLOWED. THIS IS NOT A SDR REPORTABLE EVENT PER THE GMM. ATTEMPTING
- [SDR CALA2024053101660](https://openairdocs.org/sdr/CALA2024053101660.md): Warning Light · illuminated · May 29, 2024 · N641UA · Boeing 767322 · Door Warning System
  > BULK CARGO DOOR INDICATION LIGHT AND EICAS MESSAGE ON COCKPIT. RESET BULK CARGO DOOR LIGHT AND EICAS MESSAGE, DOOR CHECKED CLOSED BEFORE DEPARTURE REF 52-71 FAULT TREE 808.
- [SDR CALA2024022900601](https://openairdocs.org/sdr/CALA2024022900601.md): Support Frame · corroded · Feb 28, 2024 · N641UA · Boeing 767322 · Fuselage Main, Structure
  > GENERATING ITEM: 166320-0100.0168, SUPPORT TASK: FLC UPPER FRAME CHORD CORRODED @ F.S. 522-544 RBL24.26. REMOVED AND REPLACED FLC UPPER FRAME CHORD SRM 523-544 RBL 24-46 IAW B767 SRM 51-40-02 PARA 7.
- [SDR CALA2024022900599](https://openairdocs.org/sdr/CALA2024022900599.md): Failsafe · corroded · Feb 28, 2024 · N641UA · Boeing 767322 · Fuselage Main, Structure
  > GENERATING ITEM: 63-5310-1-2503, FLC DOOR CUTOUT LWR SILL F/S 569 FAIL SAFE STRAP HAS CORROSION AT CARGO STOP AFT FASTENER LOCATION, TAG# 8138. LEFAIVE REMOVED AND REPLACED FAIL SAFE STRAP IAW B767 SRM 51-40-02 SECTIONS 4 & 7.
- [SDR CALA2024022800590](https://openairdocs.org/sdr/CALA2024022800590.md): Door Sill · corroded · Feb 27, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GENERATING ITEM: 63-5310-1-2503, FLC DOOR CUTOUT LWR SILL F/S 498 FLOOR STUB FRAME END SPLIT RBL 40-42, TAG# 8122. LEFAIVE.
- [SDR CALA2024022800577](https://openairdocs.org/sdr/CALA2024022800577.md): Door Sill · corroded · Feb 26, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LWR SILL F/S 553-560 INNER CHORD EXFOLIATED. TAG# 7125 (N/R 0100-0147 SAME AREA) LEFAIVE. REMOVED AND REPLACED FLC DOOR CUTOUT LOWER SILL INNER CHORD PN-143T5204-4 AT F/S 553-560 IAW B767 SRM 51-40-02 PARA 7 WORK COMPLETION EC/RA 5300-03068.
- [SDR CALA2024022800576](https://openairdocs.org/sdr/CALA2024022800576.md): Panel · corroded · Feb 26, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC BILGE CORRODED F.S 497-537 RBL 25-38. REMOVED AND REPLACED BILGE PANEL PN 143T5014U17 AT F/S 497-537 RBL 25-38 IAW B767 SRM 51-40-02 PARA 7.
- [SDR CALA2024030100619](https://openairdocs.org/sdr/CALA2024030100619.md): Floor Support · corroded · Feb 24, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LWR SILL F/S 5 41 RBL 42 FLOOR WEB SUPPORT EX FOLIATED, REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTALL @ F/S 541 RBL42 IAW B767-300 SRM 51-40-02 PAR 7 AND AMES DOC 47594 FAB 04 REV: IR.
- [SDR CALA2024030100618](https://openairdocs.org/sdr/CALA2024030100618.md): Door Sill · corroded · Feb 24, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LWR SILL F/S 6 10 RBL 40 - 42 FLOOR BEAM CHORD LWR LEG SPLIT, REPLACED FLOOR BEAM CHORD AT FS 610 EBL 40-42 IAW B767 SRM 51-40 -02 PARAGRAPH 7.
- [SDR CALA2024022800592](https://openairdocs.org/sdr/CALA2024022800592.md): Floor Support · corroded · Feb 24, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC BS 544-5 66 RBL 23.20 FLOOR SUPPORT INTERCOASTAL IS CORRODED. REMOVED & REPLACED INTERCOSTAL AT STA 544-566 RBL 23.20 IAW B767 SRM 51-40-02 UNITED EC/RA 5328-01000.
- [SDR CALA2024022800579](https://openairdocs.org/sdr/CALA2024022800579.md): Floor Support · corroded · Feb 24, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LWR SILL F/S 551 RBL 41 STRAP UPPER SURFACE CORROSION AT SCREW HOLE, BLENDED, FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED PANEL SUPPORT IAW B767 SRM 51-40-02, AMES DOC# 47594FAB02.UNITED EC/RA 2552-01302.
- [SDR CALA2024022600527](https://openairdocs.org/sdr/CALA2024022600527.md): Panel · corroded · Feb 23, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM; 166320-0100-0137 /// SUPPORT TASK, FLC BILGE PANEL CORRODED FS 537-600 RBL 25-38.
- [SDR CALA2024022600526](https://openairdocs.org/sdr/CALA2024022600526.md): Door Sill · corroded · Feb 23, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM; 63-5310-1-2503 /// FLC DOOR CUTOUT LWR SILL FS 556-562 RBL 37 FLOOR INTERCOSTAL HAS CORROSION AROUND NUTPLATE PLUS 1 N UTPLATE IS MISSING TAG NO 7127. REMOVED AND REPLACED STRAP PN-143T5014-33 AT FLC DOOR CUTOUT LOWER SILL F/S 556-562 RBL 37 IAW B76
- [SDR CALA2024022600523](https://openairdocs.org/sdr/CALA2024022600523.md): Web · corroded · Feb 23, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM 166320-0100-0137 /// SUPPORT TASK: FLC BILGE PANEL CORRODED @ FS 600-632 RBL 25-38.
- [SDR CALA2024022600524](https://openairdocs.org/sdr/CALA2024022600524.md): Support Angle · corroded · Feb 23, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM 63-5310-1-2503 /// FLC DOOR CUTOUT LWR SILL F/S 598 RBL REMOVED AND REPLACED SUPPORT ANGLE @ F/S 589 RBL 42 IAW B767-300 SRM 51-40-02 PAR 7
- [SDR CALA2024022200503](https://openairdocs.org/sdr/CALA2024022200503.md): Angle · corroded · Feb 21, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LOWER SILL F/S 566 RLB 41 "L" ANGLE UPPER SURFACE HAS CORROSION. REF AMES (ILN) NRC 166320-0100-0148. REMOVED AND REPLACED "L" ANGLE AT F/S 566, RBL 41 IAW B767 SRM 51-40-02, PAR 7. REF AMES (ILN) NRC 166320-0100-0148.
- [SDR CALA2024022200498](https://openairdocs.org/sdr/CALA2024022200498.md): Angle · corroded · Feb 21, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC DOOR CUTOUT LOWER SILL F/S 536 INNER CHORD AND BEAM "L" ANGLE HAVE UPPER SURFACE FRETTING, TAG #8126. REF AMES (ILN) NRC 166320-0100-0142. REMOVED AND REPLACED "L" ANGLE AT F/S 536 IAW B767 SRM 51-40-02, PAR 7.
- [SDR CALA2024021600436](https://openairdocs.org/sdr/CALA2024021600436.md): Heat Shield · cracked · Feb 14, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > #1 PYLON HEAT SHIELD PAN ASSY UPPER WEB CRACKED NEAR DRAIN HOLE AND AT AFT END. REF AMES (ILN) NRC 166320-0400-0175. NEW WEB FABBED AND INSTALLED IAW AMES DOC # 47594FAB01 AND UNITED EC/RA 5456-01044. FORM# 46-0024 C/W. REF AMES (ILN) NRC 166320-0400-0175.
- [SDR CALA2024021500425](https://openairdocs.org/sdr/CALA2024021500425.md): Plate · worn · Feb 14, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > #2 I/B PYLON PANEL 447AL HAS WEAR MARK INTO PANEL AROUND 2 FWD HOLES. ALSO, FLAT SEAL IS NOT CORRECT SEAL. BULB SEAL SHOULD GO THE LENGTH OF THE PANEL. REF AMES (ILN) NRC 166320-0400-0050. #2 I/B PYLON PANEL 447AL BLENDED AND FOUND TO BE OUT OF LIMITS. PARTIAL
- [SDR CALA2024021500424](https://openairdocs.org/sdr/CALA2024021500424.md): Web · cracked · Feb 14, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON MOST AFT CLOSE OUT WEB IS CRACKED. REF AMES (ILN) NRC 166320-0400-0166. NEW CLOSEOUT WEB P/N 313T3355U233 INSTALLED (M&E 76-7831-3-0155). SEE PARTIAL WORK ACCOMPLISHED ON BACK FOR MORE DETAILS, IAW B767-300 SERM 51-40-02. FORM 46-0024 COMPLETED (SSFR)
- [SDR CALA2024021600438](https://openairdocs.org/sdr/CALA2024021600438.md): Access Panel · mechanic error · Feb 9, 2024 · N641UA · Boeing 767322 · Leading Edge Devices
  > WHILE GIVING OK TO CLOSE, FOUND NR 7 SLAT INTERNAL ACCESS PANEL 612DB TO HAVE A MISDRILLED FASTENER HOLE. REPORTED BY V932171 FABRICATED NEW PART FOR #7 SLAT PANEL 612DB IAW BOEING DWG# 114T3161. INSTALLED ON J/C 166319-0600-0090. SEE BACK AND PARTIAL WORKSHEE
- [SDR CALA2024021600437](https://openairdocs.org/sdr/CALA2024021600437.md): Angle · cracked · Feb 9, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON HEAT SHIELD PAN ASSY UPPER WEB STIFFENER ANGLE CRACKED ( ANGLE LOCATION IS JUST AFT OF DRAIN HOLE) REPORTED BY V921225 NEW ANGLE P/N 313T3355-315UAL WAS FABBED ON CRO WO# C/W. 166323-0400-0003. HOLES LOCATED AND WAS INSTALLED ON NR 0400-0162 AND 040
- [SDR CALA2024021400422](https://openairdocs.org/sdr/CALA2024021400422.md): Floor Support · corroded · Feb 9, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM; 166320-0100-0137 FLC FLOOR SUPPORT INTERCOASTAL CORRODED @ F.S. 478-497 RBL 30.95 PART WAS REMOVED ON NR 0100-0137 ENT RY NO 5
- [SDR CALA2024021400421](https://openairdocs.org/sdr/CALA2024021400421.md): Web · corroded · Feb 9, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP OF FLOOR STRUCTURE AT AFT IB CORNER OF LAV A AT STA 280.
- [SDR CALA2024021200377](https://openairdocs.org/sdr/CALA2024021200377.md): Angle · cracked · Feb 8, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON INSIDE I/B ARROW HEAD PANEL AT AFT END, L ANGLE IS CRACKED. REF AMES (ILN) NRC 166320-0400-0162. REMOVED DAMAGED ANGLE AND INSTALLED NEW PN 313T3355-287 UAL. SEE CWO NO 166327-0400-0002 FOR PART FAB IAW B767-300 SRM 51-40-02. SEE PARTUIAL WORK ON BAC
- [SDR CALA2024021200375](https://openairdocs.org/sdr/CALA2024021200375.md): Strap · cracked · Feb 8, 2024 · N641UA · Boeing 767322 · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON AFT V WEB AFT STRAP WHERE STRINGER PANEL ATTACHES IS CRACKED. INSTALLED NEW STRAP PN 313T3380-660 IAW B767-300 SRM 51-40-02. S EE PARTIAL WORK ACCOMPLISHED FOR MORE DETAILS FORM 46-0024 (SSFR) SEE NON-ROUTINE 166320-0400-0168 FOR DETAILS
- [SDR CALA2024020700342](https://openairdocs.org/sdr/CALA2024020700342.md): Angle · cracked · Feb 2, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > GEN ITEM: 63-5310-1-2623. FLOOR SUPPORT BRACKET LOOKS CUTOUT/ BROKE IN TWO PLACES UNDER FLOOR BOARD 2ND IB AT R1 DOOR AT STA 287. REMOVED AND REPLACED BROKEN CAP ANGLE AT STA 287 RBL 39.25 IAW B767 SRM 51-40-02 PARA 7.
- [SDR CALA2024020200300](https://openairdocs.org/sdr/CALA2024020200300.md): Floor Support · corroded · Feb 1, 2024 · N641UA · Boeing 767322 · Fuselage Miscellaneous Structure
  > FLC FLOOR SUPPORT INTERCOSTAL CORRODED F.S. 524-541 RBL 33.08.

Next page: https://openairdocs.org/aircraft/N641UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N641UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N641UA/reports

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